IRIDIUM 106, 41917
Orbit data source: Space-Track
IRIDIUM 106, 41917 is a payload satellite owned by Iridium (US) in LEO that was launched on Sat, 14 Jan 2017 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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41917 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
OATK SSG Gilbert
Mission
Operational Commercial Communications
Bus & Motor
ELITEBUS, Unknown motor
Mass
860 kg wet, 700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Box + 2 Pan, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 IRIDIUM 106
1 41917U 17003A 26309.65581297 .00000209 00000-0 67654-4 0 9999
2 41917 86.4003 29.3886 0002307 102.5486 257.5968 14.34218108513484Epoch: 2026-11-05T15:44Z
TLE epoch observation values (Epoch: 2026-11-05T15:44:22.240Z)
Latitude
-0.00003°
Longitude
108.40928°
Altitude
781.072 km
Speed
7.463 km/s
True Right ascension
01h 57m 33s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
09:08:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.281 km
Perigee altitude
772.98 km
Semi-major axis
7,152.767 km
Eccentricity
0.00023
Inclination
86.4003°
RAAN
29.3886°
Arg. of periapsis
102.5486°
True anomaly
257.57098°
Mean anomaly
257.5968°
Eccentric anomaly
257.58389°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000067654
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Other satellites on launch #3 in the year 2017 (2017-01-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.IRIDIUM 106 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-11-06 17:25:10.261Z | 1.518° NNE | 2026-11-06 17:30:10.261Z | 64.418° ENE | 71.515° | 2026-11-06 17:35:10.261Z | 171.208° S |
| 5 mins | 2026-11-07 04:44:10.261Z | 104.574° ESE | 2026-11-07 04:46:10.261Z | 77.802° E | 17.124° | 2026-11-07 04:49:10.261Z | 41.498° NE |
| 8 mins | 2026-11-07 06:23:10.261Z | 207.962° SW | 2026-11-07 06:26:10.261Z | 270.262° WNW | 51.857° | 2026-11-07 06:31:10.261Z | 351.668° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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